Airfoil database search
Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.
(goe392-il) GOE 392 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 392 airfoil Max thickness 10.2% at 30% chord Max camber 4.8% at 40% chord Max Cl/Cd 125.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fx6617a2-il) FX 66-17AII-182 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 66-17AII-182 airfoil Max thickness 18.2% at 33.9% chord Max camber 3.8% at 37.1% chord Max Cl/Cd 125.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe380-il) GOE 380 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 380 airfoil Max thickness 6.6% at 30% chord Max camber 5.6% at 30% chord Max Cl/Cd 125.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe596-il) GOE 596 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 596 airfoil Max thickness 9.8% at 30% chord Max camber 4% at 40% chord Max Cl/Cd 125.7 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe611-il) GOE 611 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 611 airfoil Max thickness 12.9% at 29.9% chord Max camber 5.8% at 39.9% chord Max Cl/Cd 125.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe239-il) GOE 239 (MVA H.31) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 239 (MVA H.31) airfoil Max thickness 11.2% at 19.8% chord Max camber 6% at 39.8% chord Max Cl/Cd 125.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e334-il) EPPLER 334 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E334 flying wing airfoil Max thickness 11.9% at 30.3% chord Max camber 4% at 25.4% chord Max Cl/Cd 125.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(usa35b-il) USA-35B AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | USA-35B airfoil Max thickness 11.6% at 30% chord Max camber 4.1% at 40% chord Max Cl/Cd 125.6 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe478-il) GOE 478 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 478 airfoil Max thickness 13.4% at 29.6% chord Max camber 4.3% at 39.6% chord Max Cl/Cd 125.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e193-il) E193 (10.22%) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E193 low Reynolds number airfoil Max thickness 10.2% at 31% chord Max camber 3% at 44.7% chord Max Cl/Cd 125.5 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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